FLAPPING WING DRIVE MECHANISM OF FLAPPING WING-TYPE AIRCRAFT
A flapping wing drive mechanism of a flapping wing-type aircraft, comprising a power mechanism (21) mounted on a frame (11) of the aircraft, a rotatable flapping wing drive cam (31) provided with a cam curve groove (32), and a cam roller (33) which is arranged in the cam curve groove (32), which can...
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Format: | Patent |
Sprache: | chi ; eng ; fre |
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Zusammenfassung: | A flapping wing drive mechanism of a flapping wing-type aircraft, comprising a power mechanism (21) mounted on a frame (11) of the aircraft, a rotatable flapping wing drive cam (31) provided with a cam curve groove (32), and a cam roller (33) which is arranged in the cam curve groove (32), which can roll on a cam curve in the cam curve groove (32), and which is used for connecting a flapping wing drive arm (42) of a wing to a cam roller supporting shaft (34) on the cam roller (33) for linkage; and the power mechanism (21) drives the flapping wing drive cam (31) to rotate, and the cam roller (33) rolls in the cam curve groove (32) so that the flapping wing drive arm (42) and the wing connected to the flapping wing drive arm are driven to complete a flapping wing cycle in an up-down amplitude.
L'invention concerne un mécanisme d'entraînement d'ailes battantes d'un aéronef de type à ailes battantes, comprenant un servomécanisme (21) monté sur un cadre (11) de l'aéronef, une came d'entraînement en rotation (31) d |
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